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BY ORDER OF THE SECRETARY OF THE AIR FORCE AIR FORCE ...

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16<br />

AFMAN 11-217V1 3 JANUARY 2005<br />

required to ensure the power setting remains constant.<br />

1.2.3.2. Power. From experience in an aircraft, you know approximately how far to<br />

move the throttles to change the power a given amount. Therefore, you can make<br />

power changes primarily by throttle movement and then crosscheck the indicators to<br />

establish a more precise setting. The key is to avoid fixating on the indicators while<br />

setting the power. Knowledge of approximate power settings for various flight<br />

conditions will help you prevent over-controlling power.<br />

1.2.4. Trim Technique.<br />

1.2.4.1. Proper trim technique. Proper trim technique is essential for smooth and<br />

precise aircraft control during all phases of flight. By relieving all control pressures,<br />

you will find it is much easier to hold a given attitude constant and you will be able to<br />

devote more attention to other cockpit duties.<br />

1.2.4.2. Trimming an aircraft. Trim the aircraft by applying control pressures to<br />

establish a desired attitude and then adjust the trim so the aircraft will maintain that<br />

attitude when the flight controls are released. Trim the aircraft for coordinated flight<br />

by centering the ball of the turn and slip indicator using rudder trim in the direction<br />

the ball is displaced. Differential power control on multi-engine aircraft is an<br />

additional factor affecting coordinated flight. Use balanced power or thrust, when<br />

possible, to aid in maintaining coordinated flight.<br />

1.2.4.3. Changes. Changes in attitude, power, or configuration will in most cases<br />

require a trim adjustment. Independent use of trim to establish a change in aircraft<br />

attitude invariably leads to erratic aircraft control. Smooth and precise attitude<br />

changes are best attained by a combination of control pressures and trim adjustments.<br />

Trim adjustment, correctly used, is an aid to smooth aircraft control.<br />

Figure 1.2. Instrument Cross-Check Technique.

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